|Publication number||US5902379 A|
|Application number||US 08/817,714|
|Publication date||May 11, 1999|
|Filing date||Jul 29, 1996|
|Priority date||Aug 16, 1995|
|Also published as||CA2202792A1, DE69602419D1, DE69602419T2, EP0785904A1, EP0785904B1, WO1997007053A1|
|Publication number||08817714, 817714, PCT/1996/1845, PCT/GB/1996/001845, PCT/GB/1996/01845, PCT/GB/96/001845, PCT/GB/96/01845, PCT/GB1996/001845, PCT/GB1996/01845, PCT/GB1996001845, PCT/GB199601845, PCT/GB96/001845, PCT/GB96/01845, PCT/GB96001845, PCT/GB9601845, US 5902379 A, US 5902379A, US-A-5902379, US5902379 A, US5902379A|
|Inventors||Robert John Phillips, Adrian Simons|
|Original Assignee||Normalair-Garrett (Holdings) Limited|
|Export Citation||BiBTeX, EndNote, RefMan|
|Patent Citations (14), Referenced by (25), Classifications (18), Legal Events (4)|
|External Links: USPTO, USPTO Assignment, Espacenet|
This invention relates to an oxygen generating device and to a system incorporating an oxygen generating device.
In order for passengers or aircrew in an aircraft to breath when exposed to ambient atmospheric pressure at elevated altitudes, it is necessary to provide a supply of breathing gas enriched with oxygen.
One means of achieving this is to carry within the airframe a supply of compressed oxygen gas, but particularly in a small aircraft, where space is at a premium, and/or in an aircraft where the added weight of the gas bottle containing the compressed oxygen gas is significant, this is not acceptable.
To reduce weight and space requirements another means is to carry within the airframe liquid oxygen. Liquid oxygen systems give rise to space and weight penalties and also a requirement for liquid oxygen to be available for replenishment of the liquid oxygen supply at a ground station.
More recently oxygen-enriched gas has been produced on-board of the aircraft by a so-called on-board oxygen generating system (OBOGS) based on pressure swing technology using a zeolite molecular sieve material to separate oxygen from air. This requires at least two zeolite beds which have to be sequentially cycled through on-stream/generating and off-stream/purge cycles. A limitation of such systems is that theoretically the maximum oxygen concentration obtainable in the product gas is 95% unless additional means are provided for the removal of argon and other trace gases from the supply air which is normally bleed air from a compressor stage of an engine powering the aircraft.
Increasing attention is now being given to ceramic membrane technology in provision of a system which will generate substantially 100% oxygen product gas or highly oxygen-enriched product gas of breathable quality for use in aerospace and other breathing applications. Such gas will hereinafter be referred to as being "oxygen rich", and the residual gas, will be referred to as being "oxygen depleted".
Certain ceramic materials, which are so-called ionic conductors of oxygen, become electrically conductive at elevated temperatures due to the mobility of oxygen ions within the crystal lattice. Since these materials are only conductive to oxygen ions, an external electric circuit providing electronic conduction is needed. Temperatures in the order of at least 600 K are required to obtain sufficient ionic conductivity.
Such ceramic oxygen generating devices may comprise one or more ceramic membranes through which an electrical current is passed, whilst ambient air is supplied to one face of the membrane which allows oxygen in the supply air to diffuse through the membrane by ionic transport when the membrane is at the required elevated temperature, and be recovered on the other side of the membrane.
To ensure that the ambient air entering the device does not cool the membrane and prevent it from efficiently being heated to a minimum operating temperature, the ambient supply air is pre-heated typically by passing the supply air through a heat exchanger to which hot oxygen rich gas and/or hot oxygen depleted gas delivered from the oxygen generating device is fed, so that the cooler ambient air is heated.
The electrical current passing through the material has a heating effect on the material and on the air passing through the device, and at least after an initial warm up period, the oxygen generating device is self sustaining at a temperature above the minimum operating temperature at which air is separated into its oxygen rich and oxygen depleted gas components.
The amount of ambient air fed to the oxygen generating device, (and electrical current passed through the material) can be controlled as necessary, to ensure that the demand for the oxygen rich gas supply is met, but in previous arrangements it has been necessary to provide complex active control means to control the electrical current and hence the temperature of the device, so that overheating of the oxygen generating device is avoided.
With at least some commonly used ceramic membrane materials, there is a higher electrical resistance through the material at lower temperatures, and so the magnitude of electrical current which can pass through the material to cause a heating effect, is dependent on the temperature of the material, which in turn depends at least in part on the temperature of the gas mixture delivered to the material. The inventors have realised that this property of the material can be utilised to avoid overheating of the oxygen generating device without an active control means being required to control the electrical current.
According to a first aspect of the invention we provide an oxygen generating device to which a gas mixture containing oxygen is fed, and which is operable to separate the gas mixture into oxygen rich and oxygen depleted gas components, the device comprising a negative temperature coefficient of resistance material which is active at an elevated temperature above a minimum operating temperature, to separate the gas mixture into oxygen rich and oxygen depleted gets components, there being means to pass an electrical current through the device to produce a heating effect within the device to heat the gas mixture at least towards the minimum operating temperature, wherein the device comprises a plurality of active sections through each of which the gas mixture passes in turn and the electrical current supply is connected to each of the sections so that the sections electrically are in series.
Thus the electric current passing through any of the active sections, is limited by the active section with the highest electric resistance, which in general will be the coolest section.
Particularly where heated oxygen enriched and/or oxygen depleted gas from the device is used to preheat the gas mixture fed to the device, the device can be thermally managed, at least when the temperature of the device is above the minimum operating temperature, by a less complex thermal control system than would otherwise be required, to ensure that overheating of the device does not occur.
One or each of the active sections of the device may comprise a second material which when electrical current passes therethrough produces a heating effect within the device to heat the gas mixture at least when the gas mixture is it a temperature below the minimum operating temperature.
Thus there is no need to provide any separate preheating means to provide for rapid warm up of the oxygen generating device. The second material may comprise a positive temperature coefficient of resistance material, the heating effect of which may decrease as the temperature within the device increases towards the minimum operating temperature.
Hence on start-up, the second material will conduct the electric current thus to provide a heating effect to the gas mixture passing through the oxygen generating device. As the device warms up, the heating effect of the second material may decrease, but the heating effect of the first material will increase, and the first material can then become active to cause separation of the oxygen rich and oxygen depleted gas components of the gas mixture passing into the device.
According to a second aspect of the invention, we provide an oxygen generating system including an oxygen, generating device according to the first aspect of the invention. The system may include a heat exchanger through which the gas mixture passes prior to being fed to the oxygen generating device, there being passage means for heated oxygen depleted gas component and/or oxygen rich gas component from the oxygen generating device to be fed to the heat exchanger such that the gas mixture is preheated by heat exchanged from the oxygen depleted gas component and/or the oxygen rich gas component.
The system may include a control means to control the amount of gas mixture fed to the oxygen generating device, and to control the current supply to the device thereby to achieve a desired rate of production of oxygen rich gas component.
The invention will now be described with reference to the accompanying drawings in which:
FIG. 1 is a diagrammatic illustration of an oxygen generating system incorporating an oxygen generating device in accordance with the invention;
FIG. 2 is an illustrative sectional view of one embodiment of an oxygen generating device in accordance with the invention;
FIG. 3 is a diagrammatic exploded view of the embodiment of FIG. 2 showing the respective, air, current and oxygen paths through and in the device;
FIG. 4 is a diagrammatic illustrative view in cross section to an enlarged scale of part of the oxygen generating device of FIG. 2;
FIG. 5 is a diagrammatic illustrative view on an alternate embodiment;
FIG. 6 is a graph showing the relative conductivities of first and second materials which may be used within an oxygen generating device in accordance with the invention, as conductivity varies with temperature.
Referring to FIG. 1, there is shown an oxygen generating system 10, which has at its heart, a ceramic membrane module 11 being an oxygen generating device in accordance with the invention.
A gas mixture such as for example ambient air from an uncompressed compartment of an aircraft, enters the system through an inlet 12, where any debris entrained in the inlet 12 is filtered from the ambient air by a filter 13. The air is drawn into the inlet 12 and is fed through the remainder of the system via a fan 14 the speed of which is controlled by an electrical control unit 15 as hereinafter described.
The ambient air which may be at a very cool temperature indeed, possibly below 273 K then passes through a heater module 16 which will be described in more detail hereinafter, where, at least after the system 10 has warmed up, the ambient air will be pre-heated before the air passes into the ceramic membrane module 11.
The ceramic membrane module 11 generates oxygen rich gas component as hereinafter described, which passes from the module 11 via an outlet 17. The oxygen rich gas component passes through the heater module 16 via line 17a where at least some of its heat is dissipated to the ambient air, so that a cooled oxygen rich gas supply is obtained, which is fed via line 18a to a plenum 18, and hence to a filter 19 where any residual debris is removed, from which filter 19 the oxygen gas component may pass to, for example, an aircrew where the oxygen rich air component can be breathed, particularly at ambient atmospheric pressure at elevated altitudes.
The volume of the plenum 18 may be adjusted as required, but generally is of a small volume being the equivalent to perhaps, the volume of line 18a from the heater module 16 to the filter 19.
The ceramic membrane module 11 also produces a supply of hot oxygen depleted gas component which passes from the module via an outlet 20. The hot oxygen depleted air component is also fed to the heater module 16, along a line 20a, where at least some of its heat is dissipated to the ambient air passing through the heater module 16. The cooled oxygen depleted gas component then passes from the heater module 16 via line 16b and is disposed of, for example through an external port 16c of the aircraft.
The heater module 16 may also comprise an electrical resistance or some other kind of auxiliary heater so that during an initial warm up period, the ambient air entering, the heater module 16 can be warmed so that warmed air is fed to the ceramic membrane module 11 rather than cold air but in the examples to be described, preheating of the ambient air is achieved in the ceramic membrane module 11.
It will be appreciated from the discussion below that the ceramic membrane module 11 can only operate to separate the ambient air into its oxygen rich and oxygen depleted air components, when at a temperature above a minimum operating temperature; typical operating temperatures are in the range 1100-1200 K. The temperature of the ambient air within the heater module 16, and/or the temperature of the oxygen rich and/or oxygen depleted gas component within the heater module 16, is monitored, so as to provide a suitable input via line 23 to the electronic control unit 15. Also, the temperature within the ceramic membrane module 11 may be monitored, so as to provide an input 24 to the electronic control unit 15 although as will be appreciated from the discussion below, such an input 24 is not required to protect the ceramic membrane module 11 from overheating.
The pressure of the oxygen rich gas component supply in plenum 18 is also monitored, so as to provide an input 25 to the electronic control unit 15.
The speed of the fan 14, and hence the volume of air being delivered to the heater module 16 and subsequently the ceramic membrane module 11, is monitored and an input 26 is provided to the electronic control unit 15.
In response to demand for oxygen rich gas the electronic control unit 15 controls the speed of the fan 14 via a line 27, and the power fed to the ceramic membrane module 11 via a line 28 to control the level of oxygen generation in the ceramic membrane module 11. There is also a built in test which results in an output indicated at 29 for example, to alert an aircrew to the fact that the system 10 is not operating correctly.
Operation of the ceramic membrane module 11 will now be described in more detail with reference to FIGS. 2 to 4.
Referring first to FIG. 2, the ceramic membrane module 11 comprises a housing 30 which his a passage 35 for gas therethrough. The passage has an inlet 31, a first flow reverse box 32, a second flow reverse box 33, and an outlet 20 to which oxygen depleted air component is fed from the device 11 via ducting 34.
The ceramic membrane module 11 comprises a first, ceramic, material through which electrical current is passed, the material being active when at an elevated temperature above a minimum operating temperature to cause separation of air or other gas into oxygen rich and oxygen depleted gas components. Generally, the oxygen rich gas component will flow orthogonally to the oxygen depleted gas component, and both such components will flow in directions generally orthogonal to the direction in which the electrical current is flowing.
In FIG. 2, in a first passage part 35a between the inlet 31 and the first flow reverse box 32, there is first active section A comprising first material 36a in the form of a ceramic membrane stack. One suitable material consists of an electrolyte membrane such as Cerium Gadolinium Oxide (CGO) coated on both sides with an electrode made for example of Lanthanum Strontium Cobalt Ferrite (LSCF). The direction of flow of the oxygen depleted gas component is indicated at 37 (which is the same direction as the gas mixture), whilst the direction of flow of oxygen rich gas component is indicated at 38. It can be seen that direction 38 is generally orthogonal to the extent of the first passage part 35a between the inlet 31 and the first flow reverse box 32, such that the oxygen rich air component flows into a duct 39 from which it may be collected and flow from the device 11 to the outlet 17 shown in FIG. 1.
The oxygen depleted gas component flow direction is reversed in box 32, and passes into a second active section B which comprises a second passage part 35b between the flow reverse boxes 32 and 33. The second passage part 35b contains a membrane stack 36b of first material, through which the gas flows. Again, the direction of flow of the oxygen depleted component is indicated at 37, and the directions of flow of the oxygen rich gas component into duct 39 are indicated at 38.
Within a third passage part 35c between the second flows reverse box 33 and the ducting 34 for the oxygen depleted gas component, there is a third active section C comprising yet another membrane stack 36c of first material. Again the relative directions of flow of the oxygen depleted gas component and oxygen rich gas component through membrane stack 36c are indicated by arrows 37 and 38 respectively.
Referring now to FIG. 6, there is shown in full lines a graph showing how the conductivity of the first material 36a-36c changes with temperature. Below a cut-off temperature tmin it can be seen that the first material 36a-36c provides substantially no conductivity. The first material 36a-36c will fail to separate the ambient air into its oxygen rich and oxygen depleted gas components until the material 36a-36c is at a minimum operating temperature tmot.
Hence during an initial warm up period, little or no heat may be dissipated to the ceramic membrane module 11 by the first material 36a-36c as little or no electrical current will be permitted to flow therethrough because the first material 36a-36c will be substantially non-conducting.
Prior to the air passing through the first material 36a in the first passage part 35a, the air passes through a membrane stack 40a of a second ceramic material. The second material 40a may again be a ceramic material, but exhibiting a positive temperature coefficient of resistance. Suitable second material may be based on the barium titanate perovskite system.
Hence at temperatures belong tmin indicated in FIG. 6, the second material 40a will conduct electricity therethrough and thus a heating effect will be achieved in the ceramic membrane module 11. In FIG. 6, the conductivity of the second material 40a relative to temperature is indicated by the dotted lines. As the temperature within the module 11 increases, the amount of electrical current conducted by the second material 40a decreases and hence the heating effect due to the material 40a will decrease. It can be seen that it is envisaged that the conductivities of the first and second materials 36a-36c and 40a will be about equal around the temperature tmot being the minimum operating temperature, which the first material 36a-36c must attain in order to perform its function of separating the ambient air into oxygen rich and oxygen depleted gas components. This may be around 600 K.
Referring again to FIG. 2, in the second passage part 35b between the first flow reverse box 32 and the second flow reverse box 33, there is a further membrane stack of second material 40b, and in the third passage part 35c between the second flow reverse box 33 and the duct 34, there is a yet further membrane stack of second material 40c. In this embodiment, the gas mixture, as it flows through the ceramic membrane module 11, sequentially comes into contact with second material 40a, then first material 36a and so on. In another embodiment, instead of the first and second materials 36a-36c and 40a-40c being arranged in membrane stacks separate from one another as indicated in FIG. 2, the materials may be contained within a common matrix such that air passing through the ceramic membrane module 11 may simultaneously come into contact within the first and second material contained in the matrix.
The amount of oxygen rich gas component, and can be adjusted by changing the amount of electrical current which can pass through the ceramic membrane module 11, e.g. by changing the voltage across the module 11 and by adjusting the rate of delivery of ambient air to the inlet 31, by adjusting the speed of fan 14.
The temperature within the ceramic membrane module 11 is controlled by means of monitoring the temperature within the ceramic membrane module 11, and adjusting the amount of ambient air fed to the ceramic membrane module 11. In order to reduce the temperature, the speed of fan 14 is increased, thus increasing the amount of cooling air flow. In order to increase the temperature, the fan speed is reduced.
Referring now to FIG. 3 the device of FIG. 2 is shown diagrammatically with the paths of air flow and oxygen rich gas flow being indicated at 37 and 38 respectively. Other parts are labelled with the same reference numerals as in FIG. 2.
It can be seen from FIG. 3 that the electrical current is arranged to pass through the three ceramic stack active sections A, B and C in series so that there is a voltage drop across each active section A, B, C.
It has been found that utilising a single sheet membrane of first material which is active to separate the gas mixture into oxygen rich and oxygen depleted components is unacceptable in design terms and impracticable due to the required size of that sheet. Also the electrical current flow required through such a membrane to achieve adequate volumes of separation of oxygen rich and oxygen depleted gas components, is unnacceptably high.
Hence the preferred design of the device is to provide a plurality of separate stacks of active first (and second) material. Thus a practically sized device 11 can be provided and acceptably low electrical current is required.
Nevertheless there remains a problem of thermal gradients within the device, which can result in thermal stresses which could seriously damage the integrity of the device.
In accordance with the invention however the electrical current is caused to flow in series through the active sections A, B and C of the device. In this way it will be appreciated that the electrical resistance of the second active section B, the first material 36b of which is a negative temperature coefficient of resistance material, is dependent upon the temperature of the gas mixture (air) delivered to it from the first active section A of the device 11.
Hence the inventors realised that the device 11 can thermally be managed with a control system a less complex than would otherwise be required. As the temperature of air entering active section B of the device 11 increases, the resistance of the first negative temperature coefficient of resistance material 36b in active section B will decrease resulting a reduced heating effect in active section B with the result that the temperature rise of the oxygen depleted air fed through active section B of the device to active section C, will be restricted. Any increase in temperature of the air fed to active section C, could for example by a decrease in the temperature of the air fed to active section B, will cause the heating effect of the negative temperature coefficient of resistance first material 36c of the third active section C of the device to decrease, and so the heating effect of active section C and any further active sections of the device 11 will be restricted.
Hence by connecting the active sections A, B and C of the device, or at least two active sections of the device in series, the device 11 can thermally be managed at least when operating at a temperature above the minimum operating temperature of the first material 36a to 36c.
Although in the example described the first active section A is the coolest and has the higher resistance, in another arrangement, another of the active sections B,C could be arranged to have the highest electrical resistance and thus be primarily responsible for limiting the electric current through all the active sections A,B,and C.
In FIG. 4 a portion of one of the active section A of the device 11 is shown illustratively to an enlarged scale.
Passages P1-P3 for the air and oxygen depleted gas are formed by castellations of a corrugated or castellated interconnect sheets Y1 to Y3 and perforated sheets C1 to C3 being respective cathodes of the device 11 for each of the individual active layers of the stack section. Each cathode C1 to C3 forms one layer of a tri layer T1,T2,T3 which comprises the planar cathode C1 to C3, an intermediate planar electrode layer E1 to E3, which is of a first, negative temperature co-efficient of resistance material 36a and a planar anode A1 to A3.
A voltage is applied across the device between the interconnect sheet R1 and a boundary sheet R4.
Oxygen molecules contained in the gas stream within the passages P1 to P3 diffuse through the porous cathode layers C1 to C3 to the electrolyte layers E1 to E3. The applied voltage causes the oxygen molecules to ionise at the electrode layers E1 to E3. The resultant anions pass through the electrolyte layers E1 to E3 and reform at the anode layers A1 to A3, and hence pass into the passages Q1 to Q3 which extend transversely to the passages P1-P3 and are also formed by corrugations/castellations formed in a corrugated or castellated sheet Z1-Z3. Electrical current thus passes through the active section A of the device in the direction shown by arrow C through the various layers of the active section A of the device 11.
The construction shown in FIG. 4 shows a device with three layers, although more than three layers may be provided.
For an air pre-heating section, the arrangement may be similar to that of FIG. 4, but the electrolyte layers E1 to E3 would be replaced by suitable positive temperature co-efficient of resistance material (40a). The electrical potential applied across the outermost interconnect and boundary sheets A1 and A4 allows electrical current to flow through the various layers of the section of the device, when the temperature is below that required for minimum operation.
Whilst such a preheating section could be separate from the active oxygen generating section A, advantageously the sections are combined, with the sections being separated from one another by separators, such as indicated at D1 to D3 in FIG. 4.
Thus, a flow of electrical current can occur through the preheating section (or sections) and through the oxygen generating section (or sections) depending on the temperature, as indicated by the graph of FIG. 6.
By virtue of the preheating section or sections the onset of oxygen production occurs on start up, before it otherwise would. The transition between electrical current passing through the preheating section or sections and the oxygen generating section or section would ideally be instantaneous, but practically there is a transition zone where there is parallel electrical conductivity, as indicated in the graph of FIG. 6, which occurs will both the preheating and oxygen generating sections being conductive.
Various alternative constructions to that shown in FIGS. 2 to 4 are possible in which air passes separately through active sections, to which electrical current is applied, to pass in series through the sections. For example, the same principles can be applied to a tubular ceramic oxygen generating arrangement.
In FIG. 5 a flat plate design of one active section A of a ceramic membrane module 211 is shown, there being a first electrode 250 and a second electrode 251, with a matrix containing first and second material 236 and 240 between them. Ambient air passes into passageways provided between the lower plate electrode 250 and the matrix 236/240 of ceramic materials, whilst electrical current flows in the direction shown by arrow C, between one electrode 251 and the other electrode 250.
Oxygen depleted air component flows from the passageways 235 in the direction indicated by arrow D, whilst oxygen rich gas component flows from passageways in the direction shown in arrow E from the device, for use.
A plurality of such plate constructions may be arranged stacked one on top of another to provide each active section.
Hence various modifications are possible without departing from the scope of the invention. Although in the embodiments described there is in each case second material which can produce a heating effect during a warm up period, within the oxygen generating device when electrical current passes through the material to heat the gas mixture, at least when the gas mixture within the device is at a temperature below the minimum operating temperature of the first material, and possibly at temperature also below the temperature at which the first material can conduct electricity and thus dissipate heat within the oxygen generating device, the gas may be preheated by other means to above the minimum operating temperature during initial warm up.
The actual arrangement of control system of an oxygen generating system incorporating such a device may be modified compared to the arrangement shown in FIG. 1 which is given for example only. The relationship of conductivity to temperature for actual materials selected for use may not be exactly as indicated in FIG. 6.
|Cited Patent||Filing date||Publication date||Applicant||Title|
|US4174955 *||Feb 27, 1978||Nov 20, 1979||Oxygen Enrichment Co., Ltd.||Membrane oxygen enricher apparatus|
|US4198213 *||Jan 26, 1978||Apr 15, 1980||The Garrett Corporation||Self adjusting oxygen enrichment system|
|US4681602 *||Dec 24, 1984||Jul 21, 1987||The Boeing Company||Integrated system for generating inert gas and breathing gas on aircraft|
|US5108465 *||Jun 27, 1990||Apr 28, 1992||Merck Patent Gesellschaft Mit Beschrankter Haftung||Process and device for obtaining pure oxygen|
|US5119395 *||Nov 9, 1990||Jun 2, 1992||Gas Research Institute||Interlock feed-through and insulator arrangement for plasma arc industrial heat treat furnaces|
|US5169415 *||Aug 31, 1990||Dec 8, 1992||Sundstrand Corporation||Method of generating oxygen from an air stream|
|US5240480 *||Sep 15, 1992||Aug 31, 1993||Air Products And Chemicals, Inc.||Composite mixed conductor membranes for producing oxygen|
|US5261932 *||Sep 1, 1992||Nov 16, 1993||Air Products And Chemicals, Inc.||Process for recovering oxygen from gaseous mixtures containing water or carbon dioxide which process employs ion transport membranes|
|US5447555 *||Jan 12, 1994||Sep 5, 1995||Air Products And Chemicals, Inc.||Oxygen production by staged mixed conductor membranes|
|US5496388 *||Jul 1, 1994||Mar 5, 1996||Air Liquide America Corporation||System for compressing air and extracting nitrogen from compressed air|
|US5599383 *||Mar 13, 1995||Feb 4, 1997||Air Products And Chemicals, Inc.||Tubular solid-state membrane module|
|US5643355 *||Feb 7, 1996||Jul 1, 1997||Normaliar-Garrett (Holdings) Limited||Oxygen generating device|
|US5681373 *||Mar 13, 1995||Oct 28, 1997||Air Products And Chemicals, Inc.||Planar solid-state membrane module|
|JPS54101393A *||Title not available|
|Citing Patent||Filing date||Publication date||Applicant||Title|
|US6126721 *||Nov 16, 1998||Oct 3, 2000||Compact Membrane Systems, Inc.||Oxygen enriched air supply apparatus|
|US6379514 *||Oct 14, 1998||Apr 30, 2002||Robert Bosch Gmbh||Composition structure for NOx sensors|
|US6641643 *||Oct 10, 2001||Nov 4, 2003||Generon Igs Inc.||Ceramic deoxygenation hybrid systems for the production of oxygen and nitrogen gases|
|US6866701 *||Mar 21, 2003||Mar 15, 2005||Udi Meirav||Oxygen enrichment of indoor human environments|
|US7081153||Dec 2, 2003||Jul 25, 2006||Honeywell International Inc.||Gas generating system and method for inerting aircraft fuel tanks|
|US7152494 *||Jan 8, 2004||Dec 26, 2006||Honeywell Normalair-Garret (Holdings) Limited||Method of testing|
|US7279027 *||Mar 21, 2003||Oct 9, 2007||Air Products And Chemicals, Inc.||Planar ceramic membrane assembly and oxidation reactor system|
|US7306644||Jun 7, 2006||Dec 11, 2007||Honeywell International, Inc.||Gas generating system and method for inerting aircraft fuel tanks|
|US7431753 *||Jan 12, 2005||Oct 7, 2008||Matsushita Electric Industrial Co., Ltd.||Oxygen enrichment apparatus|
|US7513932||Aug 22, 2007||Apr 7, 2009||Air Products And Chemicals, Inc.||Planar ceramic membrane assembly and oxidation reactor system|
|US8161748||Mar 1, 2004||Apr 24, 2012||Clearvalue Technologies, Inc.||Water combustion technology—methods, processes, systems and apparatus for the combustion of hydrogen and oxygen|
|US8268269||Jul 23, 2007||Sep 18, 2012||Clearvalue Technologies, Inc.||Manufacture of water chemistries|
|US8409323 *||Apr 7, 2011||Apr 2, 2013||Praxair Technology, Inc.||Control method and apparatus|
|US20040112211 *||Mar 21, 2003||Jun 17, 2004||Udi Meirav||Oxygen enrichment of indoor human environments|
|US20040186018 *||Mar 21, 2003||Sep 23, 2004||Carolan Michael Francis||Planar ceramic membrane assembly and oxidation reactor system|
|US20040187613 *||Jan 8, 2004||Sep 30, 2004||Peacey David John||Method of testing|
|US20050115404 *||Dec 2, 2003||Jun 2, 2005||Honeywell International Inc.||Gas generating system and method for inerting aircraft fuel tanks|
|US20050161044 *||Jan 12, 2005||Jul 28, 2005||Matsushita Electric Industrial Co., Ltd.||Oxygen enrichment apparatus|
|US20050161339 *||Jan 24, 2005||Jul 28, 2005||Haase Richard A.||Methods and processes for the manufacture of polynucleate metal compounds and disinfectants|
|US20050198958 *||Mar 1, 2004||Sep 15, 2005||Haase Richard A.||Water combustion technology - methods, processes, systems and apparatus for the combustion of hydrogen and oxygen|
|US20070000380 *||Jun 7, 2006||Jan 4, 2007||Honeywell International Inc.||Gas generating system and method for inerting aircraft fuel tanks|
|US20080053104 *||Jul 23, 2007||Mar 6, 2008||Clearvalue Technologies||Manufacture of water chemistries|
|US20080085236 *||Aug 22, 2007||Apr 10, 2008||Air Products And Chemicals, Inc.||Planar Ceramic Membrane Assembly And Oxidation Reactor System|
|US20120255436 *||Oct 11, 2012||Collins Michael J||Control method and apparatus|
|WO2000012197A1 *||Aug 11, 1999||Mar 9, 2000||Compact Membrane Systems, Inc.||Oxygen enriched air supply apparatus|
|U.S. Classification||96/4, 95/54, 96/7, 96/9, 96/11|
|International Classification||C01B13/02, A62B7/14, B01D53/22|
|Cooperative Classification||C01B2210/0046, C01B13/0251, B01D53/22, A62B7/14, B01D2313/365, B01D63/08|
|European Classification||B01D63/08, A62B7/14, B01D53/22, C01B13/02D4B|
|Oct 6, 1997||AS||Assignment|
Owner name: NORMALAIR-GARRETT (HOLDINGS) LIMITED, UNITED KINGD
Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:PHILLIPS, ROBERT JOHN;SIMONS, ADRIAN;REEL/FRAME:008742/0073
Effective date: 19970424
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Year of fee payment: 4
|Sep 26, 2006||FPAY||Fee payment|
Year of fee payment: 8
|Oct 25, 2010||FPAY||Fee payment|
Year of fee payment: 12